Austenitic fe-cr-ni alloy for high temperature use

ABSTRACT

An austenitic alloy for high temperature use, particularly for use in resistance heating elements. The alloy includes primarily the elements Fe, Ni, and Cr, and it has the following main composition, given in weight %, Ni 38-48, Cr 18-24, Si 1.0-1.9, C&lt;0.1, and the balance Fe. The alloy provides good hot form stability, good oxidation resistance, and a relatively high electrical resistance coupled with a low change in resistance as a function of temperature.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to an austenitic Fe-Cr-Ni alloy for use at high temperatures.

2. Description of the Related Art

Austenitic Ni-base alloys containing Cr up to 30 wt %, Si up to 3 wt %, varying amounts of Fe and sometimes additions of R.E.-elements (Rare Earth) have long been used for a variety of high temperature parts up to 1100° C. service temperature. Regarding electric resistance alloys used for heating in industrial furnaces and in appliances, several alloys with varying amount of Ni are standardized in ASTM B 344-83 and in DIN 17470. These standards are not fully compatible as seen from Table 1. There are several commercial resistance alloys using variations on the theme, such as the 37-21 alloy, comprising 37% Ni, 20 to 21% Cr, 2% Si, and the balance Fe, and minor additions of rare earth elements including Yttrium (designated R.E.).

It is an object of the present invention to provide alloy compositions that combine the lower cost of a Ni content in the range, if possible, close to NiCr 30/20, i.e., 30 wt % Ni and 20 wt % Cr, with

i) a good hot form stability; and

ii) an oxidation resistance; and

iii) a relatively high electrical resistance and low change of resistance (Ct); of a higher Ni content alloy such as NiCr 60/15. TABLE 1 Summary of ASTM and DIN Standards for resistance eCr(Fe) alloys W. *) ρ Ct Nr. Cr Ni + Co Fe Al Si Mn C Other Note (μΩm) 900° C. DIN 1774 NiCr 2.4869 19-21 >75 <1.0 <0.3 0.5-2.0 <1.0 <0.15 R.E. 1.12 1.14 8020 (1.08) NiCr 2.4658 30 >60 <5.0 <0.3 0.5-2.0 <1.0 <0.10 R.E. 1.19 1.27 7030 (1.16) NiCr 2.4867 14-19 >59 19.0-25.0 <0.3 0.5-2.0 >2.0 <0.15 R.E. 1.13 1.23 6015 (1.11) NiCr 1.4860 20.0-22.0 28.0-31.0 bal 2.00-3.00 <1.5 <0.20 Only 1.04 1.28 3020 17470 NiCr 1.4843 22.0-25.0 19.0-22.0 bal 1.5-2.5 <2.00 <0.20 Only 0.95 1.24 2520 17470 ASTM 344-83 80Ni, 19-21 bal. <1.0 0.75-1.75 <2.5 <0.15 S < 0.01 1.081 20Cr 60Ni, 14-18 >57 0.75-1.75 <1.0 <0.15 S < 0.01 1.122 16Cr 35Ni, 18-21 34-37 bal 1.0-3.0 <1.0 <0.15 R.E. S < 0.01 1.014 20Cr *) Maximum 1% Co

In general, the maximum operating temperature and lifetime of an alloy increases with increased Ni-content, but several other elements have great impact on these properties as well. All of these alloys form a protective oxide layer composed of mainly Cr₂O₃, and in case of Si additions also SiO₂ to some extent. Smaller additions like rare earth elements have been used to further enhance the properties of the oxide layer, and several patents advise additions to provide a material with good oxidation life, see, e.g., EP 0 531 775 and EP 0 386 730.

In addition to good oxidation there is also a demand for good hot strength. In case of electric elements, the cost for hangers and support systems can be reduced if the material is strong enough to support its own weight, and therefore to maintain its shape at operating temperature.

For use as electric elements, the relatively high resistivity and low Ct =R_(hot)/R_(cold) ratio of resistance change from room temperature to working temperature is an important parameter. In general, the higher the Ni, the higher the resistivity and the lower the Ct factor.

Addition of elements such as Mo and W up to levels of several wt % are known to enhance the mechanical properties at high temperatures, but they are expensive and are therefore not desirable additions in applications where cost is important.

In a wide range of open coil electric resistance, heating elements, NiCr 60/15 and NiCr 30/20 type (DIN) or 60 Ni, 16 Cr and 35 Ni, 20 Cr (ASTM) alloys are used. From a cost point of view, the NiCr 30/20 or 35Ni, 20Cr type is preferred due to their lower content of expensive Ni. In applications where the watt density and therefore the element temperature are high, the oxidation life of alloys with this level of Ni has up to now been insufficient. At the same time, the mechanical properties at working temperatures have to be within acceptable limits.

SUMMARY OF THE INVENTION

The present invention relates to an alloy for high temperature use. The alloy mainly comprises Fe, Ni, and Cr and has the following main composition, given in weight %,

Ni 38-48,

Cr 18-24,

Si 1.0-1.9,

C <0.1,

and in that Fe is the balance.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows a test setup for measuring deformation of a heating coil;

FIG. 2 is a graph showing linear relationships between Si content and Ni content for an alloy in accordance with the invention and in comparison with existing alloys;

FIG. 3 is a graph showing linear relationships between Cr content and Ni content for an alloy in accordance with the invention and in comparison with existing alloys;

FIG. 4 is a graph showing additional linear relationships between Si content and Ni content for an alloy in accordance with the invention and in comparison with existing alloys; and

FIG. 5 is a graph showing additional linear relationships between Cr content and Ni content for an alloy in accordance with the invention and in comparison with existing alloys.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

It is important that the content of C is below 0.1 wt %.

Eight test melts were cast, hot rolled, and cold drawn to wire according to standard practice with chemical composition according to Table 2. TABLE 2 Chemical composition of test melts Melt # 1 2 3 4 5 6 7 8 Ni 45.5 44.2 44.3 44.8 35.0 35.0 35.3 35.2 Cr 25.4 25.3 14.9 15.0 26.5 24.8 15.0 15.0 Si 2.64 1.10 3.69 1.18 2.72 1.16 3.06 1.13 Al 0.08 0.13 0.14 0.16 0.12 0.13 0.14 0.13 N 0.04 0.05 0.02 0.02 0.04 0.04 0.04 0.02 C 0.07 0.06 0.09 0.07 0.08 0.10 0.10 0.08 S 0.001 0.002 0.001 0.002 0.003 0.002 0.002 0.002 P 0.007 0.008 0.006 0.006 0.008 0.009 0.006 0.006 Other <1 <1 <1 <1 <1 <1 <1 <1 Fe Bal. Bal. Bal. Bal. Bal. Bal. Bal. Bal.

The wires were coiled into helixes and mounted on sample holders. These were exposed to a high temperature, 950° C., by means of a laboratory furnace for 168 hours. Deformation of the helixes was measured by means of a micrometer screw according to the setup in FIG. 1.

Since these products are working at a high temperature, the oxidation life and in particular the cyclic oxidation life is an important design factor. In order to evaluate this property a cyclic oxidation test was performed. The sample wires were heated by passing electric current through them and the wires were exposed to a 2 minutes on/2 minutes off cycle. The time to burn off was recorded and the results were grouped according to performance.

A combination of the deformation performance that occurs from relatively small applied forces, such as gravity acting on, e.g., suspended heater coils, and oxidation performance at high temperature, is therefore an object of the present invention.

The results indicate that not only the level of each element, but in addition the relative contents of the base elements Nickel, Chromium, and Silicon, have a surprisingly large impact on performance. TABLE 3 Results from deformation and oxidation tests. “+’ designates a better than average result. Melt # 1 2 3 4 5 6 7 8 Sag + + + + Life + + + +

It has now been found that the relation between these elements has to be within a narrow range that is given on the one hand by sufficient deformation performance and on the other hand by adequate oxidation performance. Only in this narrow band of compositions was the optimum compromise achieved that gave the working solution.

An alloy in accordance with the invention has the main composition (in wt %) of Ni ranging from 38 to 48. The Cr level is larger than

-   -   Cr=−0.1Ni+24

and is smaller than

-   -   Cr=−0.1667Ni+30.

At the same time, the Si level is larger than

-   -   Si=1.0

and is smaller than

-   -   Si=−0.01Ni+1.9.

In FIGS. 2 and 3 the above-mentioned Si content and Cr content are shown by means of graphs, where alloys in accordance with the invention are compared with existing alloys.

The alloy can also contain up to 5% Co as a substitute for Ni and Mn up to 2%. Further, it contains Al up to 0.6%, and preferably above 0.03%, and R.E., Y, and Ca up to a level of 0.2% in total. C should be <0.1 and N in a range up to 0.15%, preferably above 0.03%. Nitride and carbide formers such as Ti, Zr, Hf Ta, Nb, and V can be added up to a total level of 0.4% but are not necessary to benefit from the advantages of the invention. The remainder consists of iron and various elements originating from the raw materials and the production process, up to a total level of <2%.

A specific example of an alloy according to the invention contains (in wt %)

-   -   Ni 39-41,     -   Cr 20-22,     -   Si 1-1.5,     -   N 0.15,     -   Ce 0.01-0.04,     -   C<0.1,     -   impurities up to 2%, and     -   Fe the balance.

Another example of an alloy in accordance with the invention having further improved oxidation performance due to the higher Ni content, but with otherwise comparable properties, is

-   -   Ni 44-46,     -   Cr 20-22,     -   Si 1-1.5,     -   N<0.15,     -   Ce 0.01-0.04,     -   C<0.1,     -   impurities up to 2%, and     -   Fe the balance.

Preferred embodiments are as follows, with the composition in weight %. In FIGS. 4 and 5 the below-mentioned Si content and Cr content are shown by means of graphs, where alloys in accordance with the invention are compared with existing alloys.

An alloy comprising

-   -   Ni 38-48,     -   Cr between −0.1Ni+23 and −0.2667Ni+36,     -   Si between 0.8 and −0.0133 Ni+2.2, and     -   Fe the balance.

An alloy comprising

-   -   Ni 40,     -   Cr 21,     -   Si 1.2,     -   N<0.15,     -   Ce 0.03,     -   C<0.1,     -   impurities up to 2%, and     -   Fe the balance.

An alloy comprising

-   -   Ni 45,     -   Cr 21,     -   Si 1.2,     -   N<0.15,     -   Ce 0.03,     -   C<0.1,     -   impurities up to 2%, and     -   Fe the balance.

Another alloy that is preferred comprises

-   -   Ni 38-48,     -   Cr larger than Cr=−0.1Ni+24 and smaller than Cr=−0.1667Ni+30,     -   Si larger than Si=1.0 and smaller than Si=−0.01Ni+1.9,     -   C<0.1,     -   Al up to 0.6, and     -   Fe the balance.

The alloy can also contain up to 5% Co as substitute of Ni

-   -   Mn up to 2,     -   Al up to 0.3,     -   R.E., Y and Ca up to a level of 0.2% in total,     -   C<0.1,     -   N<0.15,     -   Ti, Zr, Hf, Ta, Nb, and V up to a total level of 0.4,     -   <50 wt ppm S,     -   various elements originating from the raw materials and the         production process up to a total level of <2, and     -   Fe the balance.

An alternative is:

-   -   38-48 Ni,     -   18-22 Cr,     -   1.0-1.5 Si,     -   Al<0.6,     -   <0.1 C,     -   N<0.15,     -   <1 Mn,     -   <50 wt ppm S,     -   <0.5 in total sum of elements belonging to the group Ti, Zr, Hf,         Y, Rare Earth Elements (Lantanoid group), Ca, Mg, Ta,     -   <5 totally of elements belonging to the group Mo, Co, Ta, W,     -   <0.4 totally of elements belonging to the group Ti, Zr, Hf, Ta,         Nb, and V,     -   <1 of other elements arising from impurities in the melting         process, and     -   Fe the balance.

Further preferred embodiments are an alloy comprising,

-   -   Ni 39-41,     -   Cr 20-22,     -   Si 1-1.5,     -   Mn 0.5     -   C0.02,     -   N<0.15,     -   Ce 0.01-0.04,     -   impurities up to 2%,     -   and in that Fe is the balance.

And an alloy comprising,

-   -   Ni 44-46,     -   Cr 20-22,     -   Si 1-1.5,     -   Mn 0.5,     -   C 0.02,     -   N<0.15,     -   Ce 0.01-0.04,     -   impurities up to 2%,

and in that Fe is the balance. Alloys Ni Cr Si Other 353MA 35 25 1.5 N 0.17 Incoloy DS 37 18 2.3 Incoloy 800 32 21 0.5 Incoloy 617 52 22 0.5 Al 1.2 Haynes HR-120 37 25 0.6 Mb 0.7 Nikrothal 80 80 20 1.35 Nikrothal 60 57.5 16 1.5 Nikrothal 40 37 20 2 Nikrothal 30 30 21 2 Nikrothal 20 21 25 2.3 Invention ex 1 40 21 1.3 Invention ex 2 45 21 1.2

The alloy 353MA is produced by Outokumpo Oyj, Espoo, Finland. The alloy Incoloy is produced by Special Metals Corp., Huntington, W. Va., USA. The Haynes alloy is produced by Haynes International, Inc., Kokomo, Ind., USA. Nikrothal is produced by the assignee.

As is apparent from the above, the present invention fulfills the objects mentioned in the opening part of the present application. 

1. An alloy for high temperature use, and including Fe, Ni, and Cr, said alloy comprising the following, in weight %: Ni 38-48, Cr 18-24, Si 1.0- 1.9, C<0.1, and wherein the balance is Fe.
 2. An alloy in accordance with claim 1, wherein the alloy further comprises in weight %: Mn less than 2, Al, C, Ca, N, Ti, Zr, Hf, Ta, Nb, V, Mg, Ta, W, Ce, and rare earth elements together less than approximately 7, and wherein the balance is Fe.
 3. An alloy in accordance with claim 1, wherein the alloy further comprises in weight %: Cr between −0.1 Ni+23 and −0.2667 Ni+36; and Si between 0.8 and −0,0133 Ni+2.2. and wherein the balance is Fe.
 4. An alloy in accordance with claim 1, wherein the alloy further comprises in weight %: Ni 39-41, Cr 20-22, Si 1-1.5, N<0.15, Ce 0.01-0.04, C<0.1, impurities up to 2%, and wherein the balance is Fe.
 5. An alloy in accordance with claim 1, wherein the alloy further comprises in weight %: Ni 44-46, Cr 20-22, Si 1-1.5, N<0.15, Ce 0.01-0.04, C<0.1, impurities up to 2%, and wherein the balance is Fe.
 6. An alloy in accordance with claim 1, wherein the alloy further comprises in weight %: Cr between −0.1 Ni+24 and −0.1667 Ni+30, Si between 1.0 and −0.01 Ni+1.9, and wherein the alloy includes up to 5 wt % Co as a substitute for a corresponding amount of Ni, and wherein the alloy includes Mn up to 2, Al up to 0.6, rare earth elements, Y, and Ca up to 0.2% total, N<0.15, Ti, Zr, Hf, Ta, Nb, and V up to 0.4 total, S<50 wt ppm, other elements <2 total, and wherein the balance is Fe.
 7. An alloy in accordance with claim 1, wherein the alloy further comprises in weight %: Cr 18-22, Si 1.0-1.5, Al<0.6, N<0.15, Mn<1, S<50 wt ppm, wherein the alloy further includes elements selected from the group consisting of Ti, Zr, Hf, Y, Rare Earth Elements (Lantanoid group), Ca, Mg, and Ta at less than 0.5 total, and elements belonging to the group Mo, Co, Ta, W with less than 5, and elements to selected from the group consisting of Ti, Zr, Hf, Nb, and V at less than 0.4 total, wherein other elements are <2 total and wherein the balance is Fe.
 8. An alloy in accordance with claim 1, wherein the alloy further comprises in weight %: Ni 39-41, Cr 20-22, Si 1-1.5, C 0.02, N<0.15, Ce 0.01-0.04, impurities up to 2%, and wherein the balance is Fe.
 9. An alloy in accordance with claim 1, wherein the alloy further comprises in weight %: Ni 44-46, Cr 20-22, Si 1-1.5, C 0.02, N<0.15, Ce 0.01-0.04, impurities up to 2%, and wherein the balance is Fe. 